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时间:2011-03-21 08:27来源:蓝天飞行翻译 作者:admin
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25-41-41Page 403


R  **ON A/C 106-149, 153-199, 207-299, 301-399, 401-499,
 Subtask 25-41-41-865-084-A
 D. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL SERVICE IDENT. LOCATION -------------------------------------------------------------------------------2000VU LAV LIGHT 1LQ C01 2000VU LAVATORY FORWARD-HOT WATER 1MB C03 2000VU LAVATORY FORWARD-OCCUPIED 1WJ C06 2000VU WATER SYSTEM ICE PROT CTL 2DW D08 2000VU CABIN COM SYSTEM-PRAM 2RX F07 2001VU WATER SYS 1MA D02
 **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299,
 Subtask 25-41-41-010-066-C
 E. Get Access 
R R  (1) Open the lateral avionics-compartment access-door 812 (Ref. TASK 52-41-00-010-002).
 (2) Remove the wall-mounted cabin-attendant seat (Ref. TASK 25-22-41-000-001).
 (3) Remove the programming and test panel (Ref. TASK 23-73-18-000-001).
 (4) Remove the FAP (Ref. TASK 23-73-12-000-002).
 (5) Remove the floor covering as necessary (Ref. TASK 25-28-42-000-001). 
R  (6) Remove the forward passenger/crew door-frame linings (Ref. TASK 25-23-45-000-005).
 (7) Remove the cockpit door (Ref. TASK 52-51-11-000-001).
 (8) Remove the lavatory door (Ref. TASK 25-45-19-000-001).
 (9) Remove the forward utility-area ceiling-panels (Ref. TASK 25-23-42-000-001).

 EFF : ALL
25-41-41Page 404


 (10) Remove the emergency oxygen container 29WR (Ref. TASK 35-21-41-000-001).
 (11) Remove the toilet assembly (Ref. TASK 38-31-41-000-001). 
R  **ON A/C 106-149, 301-399, 401-499,
 Subtask 25-41-41-010-066-D
 E. Get Access 
R R  (1) Open the lateral avionics-compartment access-door 812 (Ref. TASK 52-41-00-010-002).
 (2) Remove the wall-mounted cabin-attendant seat (Ref. TASK 25-22-41-000-001).
 (3) Remove the FAP (Ref. TASK 23-73-12-000-007).
 (4) Remove the floor covering as necessary (Ref. TASK 25-28-42-000-001). 
R  (5) Remove the forward passenger/crew door-frame linings (Ref. TASK 25-23-45-000-005).
 (6) Remove the cockpit door (Ref. TASK 52-51-11-000-001).
 (7) Remove the lavatory door (Ref. TASK 25-45-19-000-001).
 (8) Remove the forward utility-area ceiling-panels (Ref. TASK 25-23-42-000-001).
 (9) Remove the emergency oxygen container 29WR (Ref. TASK 35-21-41-000-001).
 (10) Remove the toilet assembly (Ref. TASK 38-31-41-000-001).
 (11) Remove the toilet drain-line behind the lavatory (Ref. TASK 38-30-00-010-002).
 **ON A/C ALL
 Subtask 25-41-41-010-071
 F. Remove the lavatory smoke detector (Ref. TASK 26-17-15-000-001).

 EFF : ALL
25-41-41Page 405


 4. Procedure_________ 
R  Subtask 25-41-41-020-067 
R  A. Disconnection of the Aircraft-Interface Electrical Connections 
R  (Ref. Fig. 401/TASK 25-41-41-991-015-A) 
R  (1) In the lavatory, on the outboard wall: 
R  (a) Remove the caps, drill out the rivets and remove the access flap 
R  (1). 
R  (b) Disconnect the the electrical connectors 7200VC-A (3) and 
R  7420VC-A (2). 
R  (c) Put blanking caps on the disconnected electrical connectors. 
R  (2) Disconnect the electrical harness of the keypad 25MQ from the 
R  lavatory wall. 
R  (a) Disconnect the electrical connector 25MQ-A. 
R  (b) Put blanking caps on the disconnected electrical connectors. 
R  (c) Cut and discard the tie-wrap(s) (10) as necessary. 
R  (d) Remove the screws (7), the washers (6) and the electrical harness 
R  (9) together with the sleeve (8) and the clamps (5). 
R
 Subtask 25-41-41-020-061
 B. Removal of the AFT Sidewall Assembly. 
R  (Ref. Fig. 402/TASK 25-41-41-991-004-A)
 (1) Put the STEPLADDER 1.0 M (3.3 FT) in position.
 (2) Disconnect the electrical harness (24) of the door micro switch 2WJ.
 CAUTION : MAKE MATCH MARKS ON ALL THE ELECTRICAL WIRES BEFORE YOU_______
 DISCONNECT THEM. INCORRECT CONNECTION OF WIRES WILL CAUSE
 DAMAGE TO EQUIPMENT.
 (a) Remove the electrical wires from the terminal 7330VT (25) (Ref.
 ESPM 25-25-41).
 (b) Put blanking caps on the disconnected electrical connectors.

 EFF : ALL
25-41-41Page 406
Config-2 Aug 01/05


R R  Electrical Connections Figure 401/TASK 25-41-41-991-015-A
 EFF :  ALL  Page 40725-41-41 Config-2 Aug 01/05
 
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